Discharge through a Section for Steady Incompressible Fluid Calculator

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✖Sectional Area is the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to the axis of the beam at a point.ⓘ Sectional Area [A]			+10% -10%
✖Fluid velocity is the volume of fluid flowing in the given vessel per unit cross sectional area.ⓘ Fluid Velocity [u_f]			+10% -10%

✖Discharge is the rate of flow of a liquidⓘ Discharge through a Section for Steady Incompressible Fluid [Q]

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Discharge through a Section for Steady Incompressible Fluid

Rithik Agrawal

National Institute of Technology Karnataka (NITK), Surathkal

Rithik Agrawal has created this Calculator and 400+ more calculators!

Mridul Sharma

Indian Institute of Information Technology (IIIT), Bhopal

Mridul Sharma has verified this Calculator and 200+ more calculators!

< 11 Other formulas that you can solve using the same Inputs

Stanton Number (using basic fluid properties)

Stanton Number=External convection heat transfer coefficient/(Specific Heat Capacity*Fluid Velocity*Density) GO

Heat Loss due to Pipe

Heat Loss due to Pipe=(Force*Length*Fluid Velocity^2)/(2*Diameter *Acceleration Due To Gravity) GO

Cavitation Number

Cavitation number=(Pressure-Vapour pressure)/(mass density*(Fluid Velocity^2)/2) GO

Head Loss due to friction

Head loss=Darcy friction factor*Fluid Velocity^(2)*Length/(Pipe Diameter*2*[g]) GO

Reynolds Number for Non-Circular Tubes

Reynolds Number=Density*Fluid Velocity*Characteristic Length/Dynamic viscosity GO

Reynolds Number

Reynolds Number=Liquid Density*Fluid Velocity*Pipe Diameter/Dynamic viscosity GO

Dynamic Pressure head-pitot tube

Dynamic Pressure head=(Fluid Velocity^(2))/(2*Acceleration Due To Gravity) GO

Reynolds Number for Circular Tubes

Reynolds Number=Density*Fluid Velocity*Diameter /Dynamic viscosity GO

Inertial Force Per Unit Area

Inertial Force per unit area=(Fluid Velocity^2)*Density GO

Dynamic Pressure

Dynamic Pressure=(Liquid Density*Fluid Velocity^(2))/2 GO

Turbulence

Turbulence=Density*Dynamic viscosity*Fluid Velocity GO

< 11 Other formulas that calculate the same Output

Discharge with velocity of approach

Discharge=(2/3)*coefficient of discharging*Length*sqrt(2*[g])*(((initial height of liquid+final height of liquid)^1.5)-(final height of liquid^1.5)) GO

Discharge over a broad-crested weir for head of liquid at middle

Discharge=coefficient of discharging*Length*sqrt((2*[g])*((head of the liquid*head of liquid middle^2)-(head of liquid middle^3))) GO

Discharge over rectangle weir for Bazin's formula with velocity approach

Discharge=(0.405+(0.003/(head of the liquid+head due to Va)))*Length*sqrt(2*[g])*((head of the liquid+head due to Va)^1.5) GO

Discharge over rectangle weir with two end contractions

Discharge=(2/3)*coefficient of discharging*(Length-(0.2*head of the liquid))*sqrt(2*[g])*(head of the liquid^1.5) GO

Discharge over rectangle weir considering Francis's formula

Discharge=1.84*Length*(((initial height of liquid+final height of liquid)^1.5)-(final height of liquid^1.5)) GO

Discharge from Manning's equation

Discharge=(1/Manning’s Roughness Coefficient)*Cross sectional area*hydraulic radius^2/3*Bed Slope^1/2 GO

Discharge without velocity of approach

Discharge=(2/3)*coefficient of discharging*Length*sqrt(2*[g])*(initial height of liquid^1.5) GO

Discharge over rectangle weir considering Bazin's formula

Discharge=(0.405+(0.003/head of the liquid))*Length*sqrt(2*[g])*((head of the liquid)^1.5) GO

Discharge over a broad-crested weir

Discharge=1.705*coefficient of discharging*Length*(head of the liquid^1.5) GO

Discharge during retraction

Discharge=Velocity*(Area of piston-Area of piston rod) GO

Discharge during extension

Discharge=Velocity*Area of piston GO

Discharge through a Section for Steady Incompressible Fluid Formula

Discharge=Sectional Area*Fluid Velocity
Q=A*u<sub>f</sub>

More formulas

Mass Density at Section 1 for a Steady Flow GO

Velocity at Section 1 for a Steady Flow GO

Cross Sectional Area at Section 1 for a Steady Flow GO

Mass Density at Section 2 when flow at Section 1 for a Steady Flow is Given GO

Velocity at Section 2 when flow at Section 1 for a Steady Flow is Given GO

Cross Sectional Area at Section 2 when flow at Section 1 for a Steady Flow is Given GO

Velocity at Section when Discharge through a Section for Steady Incompressible Fluid is Given GO

Cross Sectional Area at Section when Discharge for Steady Incompressible Fluid is Given GO

What is Discharge ?

A discharge is a measure of the quantity of any fluid flow over unit time. The area is the cross sectional area across a river and the average velocity across that section needs to be measured for a unit time, commonly a minute.

How to Calculate Discharge through a Section for Steady Incompressible Fluid?

Discharge through a Section for Steady Incompressible Fluid calculator uses Discharge=Sectional Area*Fluid Velocity to calculate the Discharge, The Discharge through a Section for Steady Incompressible Fluid is defined as amount of liquid flowing through a section. Discharge and is denoted by Q symbol.

How to calculate Discharge through a Section for Steady Incompressible Fluid using this online calculator? To use this online calculator for Discharge through a Section for Steady Incompressible Fluid, enter Sectional Area (A) and Fluid Velocity (u_f) and hit the calculate button. Here is how the Discharge through a Section for Steady Incompressible Fluid calculation can be explained with given input values -> 0.006452 = 0.00645160000005161*1.

FAQ

What is Discharge through a Section for Steady Incompressible Fluid?

The Discharge through a Section for Steady Incompressible Fluid is defined as amount of liquid flowing through a section and is represented as Q=A*u_f or Discharge=Sectional Area*Fluid Velocity. Sectional Area is the area of a two-dimensional shape that is obtained when a three-dimensional object is sliced perpendicular to the axis of the beam at a point and Fluid velocity is the volume of fluid flowing in the given vessel per unit cross sectional area.

How to calculate Discharge through a Section for Steady Incompressible Fluid?

The Discharge through a Section for Steady Incompressible Fluid is defined as amount of liquid flowing through a section is calculated using Discharge=Sectional Area*Fluid Velocity. To calculate Discharge through a Section for Steady Incompressible Fluid, you need Sectional Area (A) and Fluid Velocity (u_f). With our tool, you need to enter the respective value for Sectional Area and Fluid Velocity and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Discharge?

In this formula, Discharge uses Sectional Area and Fluid Velocity. We can use 11 other way(s) to calculate the same, which is/are as follows -

Discharge=Velocity*Area of piston
Discharge=Velocity*(Area of piston-Area of piston rod)
Discharge=(2/3)*coefficient of discharging*Length*sqrt(2*[g])*(((initial height of liquid+final height of liquid)^1.5)-(final height of liquid^1.5))
Discharge=(2/3)*coefficient of discharging*Length*sqrt(2*[g])*(initial height of liquid^1.5)
Discharge=(1/Manning’s Roughness Coefficient)*Cross sectional area*hydraulic radius^2/3*Bed Slope^1/2
Discharge=1.84*Length*(((initial height of liquid+final height of liquid)^1.5)-(final height of liquid^1.5))
Discharge=(0.405+(0.003/head of the liquid))*Length*sqrt(2*[g])*((head of the liquid)^1.5)
Discharge=(0.405+(0.003/(head of the liquid+head due to Va)))*Length*sqrt(2*[g])*((head of the liquid+head due to Va)^1.5)
Discharge=(2/3)*coefficient of discharging*(Length-(0.2*head of the liquid))*sqrt(2*[g])*(head of the liquid^1.5)
Discharge=1.705*coefficient of discharging*Length*(head of the liquid^1.5)
Discharge=coefficient of discharging*Length*sqrt((2*[g])*((head of the liquid*head of liquid middle^2)-(head of liquid middle^3)))

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